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Chair: Tobias Bandi (CSEM) - Mark Ford (ESA) |
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MicroThrust "C Microsystems As A Solution To Enable High Isp Electric Propulsion For Small Spacecraft |
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Dandavino, S.1; Ataman, C.2; Chakraborty, S.2; Shea, H.2 |
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1Microsystems for Space Technologies Lab. (LMTS), SWITZERLAND; 2EPFL - Microsystems for Space Technologies Lab. (LMTS), SWITZERLAND |
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Micro Coriolis Mass Flow Sensor for Chemical Micropropulsion Systems |
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Wiegerink, R.J.1; Lammerink, T.S.J.1; Groenesteijn, J.1; Dijkstra, M.1; Lotters, J.C.2 |
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1MESA+ Institute for Nanotechnology, NETHERLANDS; 2Bronkhorst High-Tech, NETHERLANDS |
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Miniaturization of Components and Systems for Space Applications |
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Gronland, T.A.; Johansson, H.; Bendixen, M.; Salaverri, A.; Rangsten, P. |
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NanoSpace, SWEDEN |
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PRECISE - Development of a MEMS-based monopropellant micro Chemical Propulsion System |
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Gauer, M.1; Telitschkin, D.2; Gotzig, U.2; Batonneau, Y.3; Rangsten, P.4; Ivanov, M.Y.5; Palmer, P.6; Wiegerink, R.J.7 |
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1DLR - German Aerospace Center, GERMANY; 2EADS Astrium Space Transportation, GERMANY; 3University of Poitiers, IC2MP UMR CNRS, FRANCE; 4Nanospace AB, SWEDEN; 5NPO Mashinostroyenia, RUSSIAN FEDERATION; 6University of Surrey, UNITED KINGDOM; 7University of Twente, MESA+ Research Institute, NETHERLANDS |
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Performance Demonstration of THEON's Existing Pressure Modules for Space Applications |
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Athanasopoulos, T.; Glykiotis, G.; Spyropoulou, K.; Michalakou, A.; Zervakis, E. |
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THEON SENSORS SA, GREECE |
